Distance measuring device and method for determining a distance, and a suitable reflective member

ABSTRACT

A distance measuring device and a method for determining a distance are provided. The distance measuring device includes a reflective member, evaluation electronics and a sensor device having at least one coupling probe for feeding a transmission signal into a line structure with the reflective member. The reflective member includes a base plate with an attached collar for forming a cup-shaped element.

CROSS REFERENCE TO RELATED APPLICATIONS

This application claims priority to and the benefit of the filing date of PCT Application No. PCT/EP2007/007258, filed Aug. 16, 2007 and German Patent Application No. DE 10 2006 038 469.5, filed Aug. 17, 2006, both of which are each hereby incorporated by reference in their entirety.

BACKGROUND OF THE INVENTION

The present invention relates to a distance measuring device as well as to a method for determining a distance and to a suitable reflective member.

Conventional distance measuring devices are used among other things for example for detecting the piston position of fluidic linear drives and pneumatic and hydraulic cylinders. The detection of the piston position on cylinders can be implemented both discretely, i.e. at discrete points, and continuously, i.e. constantly during operation.

A discrete piston position determination is generally required in order to report back the implementation or end of a piston movement to a sequence control system (e.g. SPS) in order to, for example, be able to initiate the next sequence step.

Predominantly used for this purpose are sensors or sensor devices sensitive to magnetic fields which detect the magnetic field of a permanent magnet which is located on the cylinder piston. The sensors used are fitted externally to the cylinder tube of the piston cylinder. If the piston moves into the detection range of this type of sensor, the latter recognizes the presence of the cylinder piston through the cylinder tube. For this the use of non-ferromagnetic materials is predominantly required and so restricts the structural properties and applications of the drive.

If, however, a different position of the piston is detected, the sensor must be correspondingly mechanically adjusted. For each position to be detected in addition a further sensor must consequently be fitted, accompanied by the associated additional material, fitting, adjustment and installation costs.

This generally takes place on site (e.g., at the customer's premises). Here the cylinder is often already integrated into a machine which is difficult to access, and adjustment of the switching distances by mechanically moving the externally fitted magnetic switches is no longer possible.

Furthermore, for these externally fitted sensors additional installation space is required. So that the accessibility and robustness of the sensor can be guaranteed, additional structural complexity is often required.

These types of sensor are predominantly in the form of sensors sensitive to magnetic fields and are known as Reed switches, magnetoresistive (MR), giant magnetoresistive (GMR), Hall switches or magnet-inductive proximity switches.

Complex coordination of the magnet to the sensor device is required for detection of the magnetic field. Moreover, with this measuring principle, the possible applications are restricted by interfering static and dynamic magnetic fields (EMV, field of a nearby cylinder) and the temperature characteristics of the sensor.

For the continuous measurement of the piston position measuring systems are generally used which function potentiometrically, magnetrostrictively according to the LVDT principle (Linear Variable Differential Transformer) or according to the ultrasound principle. With these systems the piston position is emitted continuously and predominantly as an analog voltage signal. Sensors according to the LVDT principle always require a reference path when switched on. Magnetostrictive sensors are fitted either externally onto the cylinder or into a hollow piston rod. Both fitting possibilities mean substantially increased complexity, are prone to interference or weaken the stability of the drive in the case of the hollow piston rod. Ultrasound sensors are only suitable to a limited degree for the path measurement in pneumatic and hydraulic cylinders because the measuring accuracy changes with the cylinder pressure. Incremental path measurements are also known as a supplement to these systems. These systems are implemented for example by the coding of the piston rod, and so can only be used for the relative path measurement.

Neither the continuous nor the discrete piston position determination can be integrated into a cylinder or can only be so with substantial structural complexity and the associated high costs. The substantial structural complexity is due to the fact that all of the established sensor principles described must be adapted to the corresponding cylinder length because they have a detection range which is too short.

The ideal path measuring system for determining the piston position in pneumatic and hydraulic cylinders has the following properties, namely a continuous, absolute path measurement with an accuracy of 100 pm for positioning the piston, total integration of the sensor with analysis electronics into the cover of the cylinder, switching distances should be adjustable externally via an electronic interface (teach-in capability), a universally applicable sensor, independently of the cylinder length, measurement results independent of pressure, oil and humidity in the cylinder, and/or reliable measurement results, e.g. up to 10 bar pressure and 6 m/sec piston speed in the pneumatic cylinder.

Further prior art is described in patent application No. 102 05 904.7.

In practice, the measuring system described in the patent application has the following problems for cylinders with a large diameter (>50 mm): the plastic ring for the piston stop and the antenna retainer is first of all very large. These plastic parts are only available up to a maximum diameter of 60 mm as ready-made items. For larger diameters expensive custom-built models are required. Moreover, plastic absorbs water over time or releases water according to the conditions of use, and in this way changes the measuring conditions. The measurement results then become inaccurate and no longer correspond to the specification.

Classic end position damping, e.g. of the pneumatic piston can only be achieved secondly by the moved brake ring made of plastic at the expense of measuring accuracy.

Further disadvantages of the measuring system described in patent application No. 102 05 904.7 are: that the conventional pistons in the pneumatic cylinder are relatively thin and generally have a magnetic ring in the center in order to enable operation with externally fitted Reed switches. These pistons do not form an ideal reflective member for an electromagnetic wave. Part of the electromagnetic wave passes over the piston into the functional space of the cylinder lying behind this, returns with a time delay and interferes with the useful signal. This substantially worsens the measuring accuracy. Furthermore, there are pistons which are made entirely of plastic. These pistons do not constitute a reflective member at all for the electronic wave. The method described in the above patent application then no longer works at all.

Furthermore, a disadvantage of a piston stop in the cover made of plastic is that the plastic is settled by frequent piston impacts and so the physical conditions in the functional space of the cover change for the high frequency sensor. Moreover, the measuring accuracy worsens.

In addition, with smaller cylinder diameters it is very difficult to integrate the discrete electronics into the cylinder cover. Part of the electronics must then complexly be accommodated externally, e.g. on the cylinder wall.

BRIEF DESCRIPTION OF THE INVENTION

Various embodiments of the present invention provide a distance measuring device and a method for determining the distance that enables continuous and therefore discretisable distance determination, simple handling and versatile possibilities for use.

Accordingly, it is made possible by the geometric design of the reflective member for the coupling probe to plunge without any contact into the interior of the reflective member, in particular within the collar, upon deflection of the reflective member. Displacement of the position of the coupling probe is prevented and the measuring accuracy retained. Due to the presence of the collar it is possible for the deceleration process of the reflective member to be implemented with a plastic ring which does not effect the distance measurement because the plastic ring is not located within the reflective member.

Furthermore, a line structure is provided which has a feed block with a feed region which connects an HF transceiver to the coupling probe via a waveguide with dielectric restraint systems. With this arrangement, total integration of the coupling probe with the analysis electronics in the cylinder cover is possible. Therefore, additional parts to be fitted externally are not required. The corresponding switching distances can preferably be adjusted externally via the analysis electronics by means of an electronic interface. The distance measuring device can basically be used universally independently of the cylinder length. Moreover, it has been shown that the measurement results are reliably correct independently of the pressure, oil and air humidity in the cylinder.

Also, a distance measuring device and a method for determining a distance is made available, the sensor device having a high frequency feed system which serves to measure a specific distance, for example in a line structure (a line structure being e.g. the interior of the pneumatic cylinder=circular hollow conductor) by radiating and receiving waves, with, for example, the feed system being integrated into the line structure. Upon the basis of this integration of the feed system it is possible for the distance measuring device to have a small structure and for practically no or only slight structural alterations to be required. Therefore, the overall structure of the distance device can have a clean, sleek design due to dispensing with a fitting possibility for external sensor devices and does not effect the external appearance. With the distance measuring device, economy of installation is achieved because the pre-fabricated cylinder only has one connection cable for control and data collection. According to various embodiments of the method, the length of the line structure is measured up to a short circuit (e.g. piston as reflective member with the pneumatic and hydraulic cylinder) which is also moveable. The transmission signal provided according to the method is fed into a line structure and preferably reflected by a short circuit (=cylinder piston). In this way the measurement of the distance between the feed point defined by the coupling probe and the short circuit of the line structure is implemented. The distance to be measured here is implemented by measuring the phase difference between the transmitted and the received signal.

More specifically, the arrangement is provided as follows: The RF feed system comprises a coaxial monopole stimulation system. By feeding a transversally electromagnetic wave (TEM wave) in the coaxial inlet region (3) a circular hollow conductor wave with the characteristic E field type of the E01 wave is stimulated by the monopole system. This wave propagates within the running cylinder in the axial direction. If this wave strikes a reflective member (within the pneumatic and hydraulic cylinder the piston), the wave is reflected and converted and conveyed into the coaxial line system via the stimulation section (monopole). The monopole feed comprises a 3-stage coaxial transformation stage with a dielectric restraint system, for example made of PPS Gf 40 material, for positioning and pressure stabilisation.

With cylinders with a large diameter the dielectric restraint system can only be implemented partially in the form of dielectric supports. The piston end stop is formed by a base plate with an attached collar for forming a cup-shaped part made of aluminium which is fitted as an end piece onto the piston. The cup is formed such that the antenna plunges without any contact within the cup upon impact. A plastic plate is accommodated on the front face of the cup in order to enable a soft impact. This cup additionally serves as a reflective member for the transmitted electromagnetic wave. In order to achieve ideal reflection conditions, around the periphery of the reflective member so-called “corregations” are provided. These are milled grooves which constitute a short circuit for the electromagnetic wave. Depending on the number of grooves an almost perfect short circuit can therefore be produced. In practice two grooves are sufficient. The depths of the grooves correspond to a quarter of the wavelength of the transmission frequency of the electromagnetic wave used. The reflective member consists is also able to be designed in order to implement the function of end position damping. Without the end position damping the piston would strike the cover without any deceleration. This leads to jerks and can cause damage to the drive system. The classic end position damping is achieved by the piston rod projecting over the piston towards the sensor and being providing with a conically extending plastic attachment. The counterpiece in the end cover forms a plastic ring the internal diameter of which is of such a size that the piston rod can plunge with the conically extending plastic attachment. If the internal diameter of the plastic ring corresponds to that of the external diameter of the conical piston rod attachment, the piston is decelerated. In order to enable the cylinder to start up smoothly following a deceleration process, the plastic ring is mounted in the cover so that the plastic ring can move e.g. a few millimetres axially. If the piston starts up again following a deceleration process, it takes the plastic ring with it up to the stop of the latter.

Due to the kinetic energy which the piston then has, there is a gentle jolt and the plastic ring is released from the conical plastic attachment of the piston rod. The deceleration process is supported by an air exchange between the cover and the cylinder space adjustable by means of a screw. The disadvantage for the HF path measuring system is that the movement of the plastic ring within the cover space changes the physical circumstances for the sensor and the measuring accuracy consequently worsens substantially. Basically the classic end position damping can also be implemented with the proposed configuration. The plastic ring sits in the cover and the conical extension of the piston rod is provided on the reflective member. In the various embodiments, the movement of the plastic ring is now masked by the cup, i.e. the sensor signals can no longer be interfered with by the antenna plunging into the cup due to the movement of the plastic ring. Also, the work scheme may be reversed. The moveable plastic ring is now fitted onto the outer surface of the cup and the cover plunge surface is formed conically and coated in plastic. The movement of the ring over the reflective member does not effect the electromagnetic wave because the plastic ring is no longer located in the vicinity of the antenna. Likewise, the pneumatic pressure compensation is advantageously provided in the cover.

All of the plastic parts directly next to the monopole antenna in various embodiments of a plastic material with low water absorption such as e.g. PPS Gf 40.

The whole pneumatic cylinder between the piston rod and the rearward cover is observed during the process introduced e.g. as a circular hollow conductor. According to the geometric dimensions of the cylinder the transmission frequency of the sensor is chosen such that monomodal propagation of the electromagnetic wave (in the example in the E01 mode) is possible. Stimulation of hollow conductor modes of a lower order is prevented by the geometry of the feed. The stimulation of the electromagnetic wave in the cylinder is implemented e.g. via a monopole (=antenna) in the way described. According to the reflectometer principle the wave propagates in the circular hollow conductor (=pneumatic cylinder) and is reflected on the piston (=short circuit). In order to be able to measure the distance between the piston and the sensor continuously, the transmission signal must be modulated. This can take place in the form of a frequency modulation or by analysing the phase difference between the transmitted and the received signal with a number of frequencies. The transmission frequency is generally between 100 MHz and 25 GHz.

The use of a dielectric secondary ring serves as a stop safeguard for the moving reflective member and is taken into account with the electromagnetic design of the feed system.

If the line structure is a circular hollow conductor, a cylinder with a piston may be used as a reflective member. A circular hollow conductor of this type can be for example a pneumatic cylinder or a hydraulic cylinder.

Due to the presence of boreholes in the feed block into which the restraint system, the coupling probe and the coaxial feed region can be inserted, simple fitting is guaranteed and the whole distance measuring device can be integrated almost any way into existing line structures.

Additionally, a coupling probe may be provided as a monopole stimulation system and the electromagnetic wave feed is implemented coaxially so that a circular hollow conductor wave can be fed in and be converted to the monopole by means of a multi-stage coaxial transformation stage. By means of the multi-stage coaxial transformation stage, which can have a level base area on which an electrically conductive cylinder is provided in the center, and to which an electrically conductive pin is attached as an inner conductor of the coaxial feed, it is possible for the whole feed to be implemented simply.

The restraint system comprises dielectric, e.g. lexan, and is used for the positioning of the coupling probe within the cylinder. Furthermore, it provides the required mechanical stability when subjected to pressure (e.g. 10 bar in the pneumatic cylinder). During series production the feed block can be produced particularly cost-effectively by the monopole stimulation system being inserted into the cylinder cover and the dielectric restraint system connecting the system to the cylinder cover by means of the plastic injection method.

Further, an electromagnetic wave in the high frequency range of between 100 MHz and 25 GHz may be fed in. Dependently upon the dimensions and measurements of the cylinder used as the line structure and the wave mode, an appropriate frequency is chosen which is above the lower limit frequency of the wave mode used.

BRIEF DESCRIPTION OF THE DRAWINGS

By means of the following drawings embodiments of the distance measuring device are illustrated.

FIG. 1 shows a sectional illustration of a distance measuring device in an integrated line structure formed in accordance with various embodiments of the invention;

FIG. 2 shows perspectively an exploded view of the distance measuring device of FIG. 1 (left-hand side) and of the distance measuring device according to the application in the assembled state (right-hand side).

FIGS. 3-9 are individual component illustrations of the distance measuring device formed in accordance with various embodiments of the invention.

FIG. 10 is a block diagram of a high-frequency chip formed in accordance with various embodiments of the invention.

FIGS. 11 and 12 are drawings showing conventional line structures.

DETAILED DESCRIPTION OF THE INVENTION

In FIG. 1 the distance measuring device according to various embodiments is illustrated with a line structure 1 and a feed block with a feed region 2 (illustrated as 2 a-2 c), the feed region having a coupling probe 3 via a dielectric restraint system 5 with the waveguide. In addition, the dielectric secondary ring 9 is illustrated which serves on the one hand as a mechanical stop safeguard and is designed as a secondary adjustment and radiation system.

The respective components of the distance measuring device are illustrated more clearly in FIGS. 2-9, the essential components such as the feed block with a feed region 2 being reproduced in an exploded view in FIG. 2. It can also clearly be seen that the dielectric restraint system 5 holds the coupling probe 3 in the form of a monopole stimulation system which includes a pin which can be accommodated in a coaxial waveguide. In addition the dielectric secondary ring 9 is shown. Likewise, the reflective member with the attached collar for forming a cup-like element, the base plate of which advantageously has a groove structure, is shown.

For better understanding the mode of operation of the distance measuring device and of the method for determining the distance will be described more clearly.

The feed system comprises a coaxial monopole stimulation system. By feeding a transversally electromagnetic wave, i.e. TEM wave in the coaxial feed and input region, by means of the monopole system a circular hollow conductor wave with the characteristic E field type of the E01 wave is stimulated. This wave propagates within the running cylinder in the axial direction. If this wave strikes a reflective member, i.e. in the pneumatic and hydraulic cylinder the piston, the wave is reflected and converted by the stimulation section (monopole) into the coaxial line system and conveyed on to a HF transceiver (transmitting and receiving unit). The monopole feed comprises a multi-stage coaxial transformation stage as a coupling probe 3 with a dielectric restraint system 5, preferably made of PPS Gf 40 material, for positioning and pressure stabilization. With cylinders with a large diameter the dielectric restraint system can only partially be designed in the form of dielectric supports. The piston end stop is provided by means of a cup-shaped part 6 made e.g. of aluminium, which is fitted on the piston as an end piece. Here the cup is designed such that upon impact the antenna plunges without contact inside the cup. A plastic plate 7 is accommodated on the front face of the cup in order to enable a soft impact. This cup serves additionally as a reflective member for the transmitted electromagnetic wave. In order to achieve ideal reflection conditions so-called “corregations” 8 have been provided around the periphery of the reflective member. These are milled grooves which constitute a short circuit for the electromagnetic wave. Depending on the number of grooves an almost perfect short circuit can therefore be produced. In practice two grooves are sufficient. The depths of the grooves correspond to approximately a quarter of the wavelength of the transmission frequency of the electromagnetic wave used when air is located in the grooves. The depth of the grooves can be shortened substantially if the latter are filled with dielectric e.g. teflon. In practice dielectric rings may be inserted. A further embodiment of the reflective member is such that the reflective member can be formed to enable one to thus execute the function of end position damping. Without end position damping the piston would strike the cover without any deceleration. This leads to jolts and can cause damage to the drive system.

Classic end position damping is implemented in that the piston rod projects over the piston towards the sensor and is provided with a conically extending plastic attachment. The counterpiece in the end cover forms a synthetic ring the inner diameter of which is of a size such that the piston rod can plunge in with a conically extending plastic attachment. If the inner diameter of the plastic ring corresponds to that of the outer diameter of the conical piston rod attachment, the piston is then decelerated. In order to enable the cylinder to start up smoothly following a deceleration process, the plastic ring is mounted in the cover such that it can move axially e.g. a few millimeters. If the piston starts up again following a deceleration process, then the piston carries the plastic ring with it up to the latter's stop. By means of the kinetic energy which the piston then has there is a gentle jolt and the plastic ring is released from the conical plastic attachment of the piston rod. The deceleration process is supported by an air exchange between the cover and cylinder space which can be adjusted by means of a screw. The disadvantage for the HF path measuring system is that the movement of the plastic ring within the cover space changes the physical circumstances for the sensor and in this way the measuring accuracy is substantially worsened. Classic end position damping can also be implemented with the proposed configuration. The plastic ring sits in the cover and the conical extension of the piston rod is implemented on the reflective member. The advantage of this solution is that the movement of the plastic ring is now masked by the cup, i.e. the sensor signals are no longer interfered with by the plunging of the antenna into the cup by the movement of the plastic ring. An equally advantageous embodiment is achieved if the work scheme is reversed. The moveable plastic ring is now fitted onto the outer surface of the cup and the cover plunge surface is formed conically due to the application of a plastic ring. The movement of the ring over the reflective member does not effect the electromagnetic wave because the plastic ring is no longer located close to the antenna.

All of the plastic parts directly adjacent to the monopole antenna must be made of a plastic material with low water absorption such as e.g. PPS Gf 40.

A method according to various embodiments of the invention will now be described by means of a pneumatic cylinder. Here the whole pneumatic cylinder between the piston rod and the rearward cover e.g. as a circular hollow conductor will be considered. The transmission frequency of the sensor is chosen according to the geometric dimensions of the cylinder such that monomodal propagation of the electromagnetic wave (in the example in the E01 mode) is possible and that the stimulation of hollow conductor wave modes of a high order is prevented. The stimulation of hollow conductor modes of a lower order is prevented by the geometry of the feed. Stimulation of the electromagnetic wave in the cylinder takes place e.g. via a monopole in the way described. The wave propagates in the circular hollow conductor (=pneumatic cylinder) according to the reflectometer principle and is reflected on the piston (=short circuit). In order to be able to measure the distance between the piston and the coupling probe continuously, the transmission signal must be modulated. This can take place in the form of a frequency modulation. In order to achieve a high distance resolution a large frequency shift is required however. In practice, transmission of a CW signal is more advantageous, e.g. with three different frequencies (for example: 5.8 GHz, 6.0 GHz, 6.2 GHz) in order to establish a clear distance range with respective subsequent analysis of the phase difference between the transmitted and received signal as a highly accurate measured value for the distance between the coupling probe and the piston. The number of frequencies to be used and the position of the latter is first and foremost dependent upon the maximum distance to be measured and the required error tolerance in relation to the phase angle measurement. In general, with a small frequency difference between two measured frequencies the maximum measurable distance is greater, but the difference between two consecutive periods requires greater accuracy of the phase angle measurement than with a greater frequency difference. Resistance to interference is therefore higher with greater differences between the individual measuring frequencies.

If a large measuring range with sufficient resistance to interference is to be measured, a number of measuring frequencies with a suitable frequency position are required. For this reason frequency pairs both with a small difference in transmission frequency (large measuring range) and with a large frequency difference (interference resistance) are then required.

The position accuracy is substantially determined by the accuracy of the phase angle measurement with the highest measuring frequency because the wavelength is the smallest here. The following formula applies: path change=phase angle change×wavelength/180°

The piston position measurement by means of a microwave is based upon the following principle: An electromagnetic wave of an appropriate frequency is coupled into the cylinder. The cylinder itself acts as a line structure for the wave. The wave passes in the cylinder to the piston as a reflective member. On the piston the electromagnetic wave is largely reflected because the piston behaves electrically similarly to a short circuit. The reflected wave runs back to the cylinder and is uncoupled from the cylinder again by means of the same structure by means of which the coupling also took place. The phase angle between the coupled and the reflected signal is measured. If the piston changes its position, the path over which the electromagnetic wave passes within the cylinder also changes. The path change also brings about a change to the signal duration and so also another phase angle between an incoming and reflected wave. Therefore, the phase between the incoming and returning signal can be used as a measure for the piston position. The following correlation between the piston position and the phase angle p results:

$\varphi = {\frac{2x \times 360^{\circ}}{\lambda} + \varphi_{o}}$ φo here is a phase offset which is mainly determined by the supply and the coupling. It is constant and so has no effect upon the actual position measurement. The above equation also gives the required phase measurement accuracy in order to be able to achieve a pre-specified position measurement accuracy.

Since with a phase measurement one can basically not distinguish between a phase angle φ and φ+n*360°, when using just one frequency only cylinders up to a maximum piston stroke <λ/2 could be measured. When using two or more frequencies it is possible, however, to measure pistons with a substantially greater length. With two frequencies the two wavelengths must not differ too greatly. For a cylinder with length I the following applies for the wavelengths:

$\lambda_{1} > \lambda_{2} > \frac{2l\;\lambda_{1}}{{2l} + \lambda_{1}}$

Since the phase angle of the reflected signal can not be measured directly and so the voltage measured on a mixer outlet is not directly proportional to the piston position, an appropriate algorithm is required for the position search. Since the output signal is periodically repeated, it must be ensured above all that the position search runs clearly, i.e. it must be possible to determine clearly in which period the piston is located. One possibility for determining the position is to record many measured values during one frequency sweep. These measured values are then transformed by means of a FFT or DFT into the frequency range. From the position of the maximum of the spectrum produced the position of the piston can then be determined. Provided one does not allow any sub-sampling when recording the measured values, with this method no problems associated with ambiguity can occur. By means of this method values for the piston positions are obtained without recording a position table.

Disadvantageous is the fact that on the one hand a relatively large number of measurement points have to be recorded, and that the time required for calculation is relatively great.

Another embodiment includes measuring with only a few frequencies and to determine the piston position by means of position tables. The measured values are thus compared easily with the values of the points of the position table. The position established then corresponds to the table value which is most similar to the measured values. It is a disadvantage with this method that ambiguities may occur. Since direct phase measurement is not implemented, clarity can not be guaranteed by observing the condition described above. More precise investigations show that when using just two measuring frequencies there are always points with identical measured values if the cylinder is longer than A12. Since in practice this is mostly the case, one should work with at least three frequencies. If the three measuring frequencies are chosen wisely, there are then no more positions with which all three measured values are identical. However, in practice the measured values must differ by a minimum amount at two piston positions in order to be able to guarantee clarity, even with certain measuring errors. Therefore, with larger cylinder lengths in particular the use of more than three frequencies can be advantageous. Moreover, in this way the measuring accuracy is also increased because noise or measuring errors which only occur with one frequency are suppressed.

The transmitted and received signals are generated in corresponding HF electronics. For this purpose the coax conductor (=pin of the monopole) is connected via a solder joint, plug or bond connection which carries the HF electronics to the conductor board. The HF electronics are in the form of a single chip substrate made e.g. of silicium germanium. The components which are provided here are shown by the block diagram, HF chip, according to FIG. 10. An oscillator (VCO=voltage controlled oscillator) generates the high frequency signal, e.g. with 24 GHz. The oscillator frequency is stabilized by a control loop.

For this purpose the oscillator output signal is split into the frequency, e.g. by factor 16 and adjusted with quartz accuracy by means of a PLL (phase locked loop). In the transmission branch there is then a switchable divider which establishes the final transmission frequency by means of the divider ratio. With an oscillator frequency of 24 0 Hz this can be 12, 6, 3, . . . GHz. The associated power amplifier corresponding to the frequency is activated by an external circuit according to the chosen divider ratio. The signal is then radiated via the monopole antenna. After the electromagnetic wave has been reflected on the reflective member, it is received via the monopole antenna and forwarded to the receiver via two directional couplers. The receiver is in the form of an IQ receiver. According to the frequency set the intermediate frequencies of the receiver (IF out) undergo analog/digital conversion and are analyzed in an FPGA (free programmable gate array). Consequently one obtains the distance value between the sensor and the piston. The latter is passed either analoguely e.g. via a 0 to 20 mA or 0 to 10V interface or digitally e.g. CAN bus to a SPS. In the FPGA the function blocks DSP (digital signal processor), parts of the interface, memory and parts of the PLL control are provided.

It should be noted that the principle of end position damping can be implemented in reverse in the sense of a kinematic reversal, i.e. the moveable plastic ring is located in the cover and the conically extending plastic pin on the outer surface of the cup.

It is to be understood that the above description is intended to be illustrative, and not restrictive. For example, the above-described embodiments (and/or aspects thereof) may be used in combination with each other. In addition, many modifications may be made to adapt a particular situation or material to the teachings of the invention without departing from its scope. While the dimensions and types of materials described herein are intended to define the parameters of the invention, they are by no means limiting and are exemplary embodiments. Many other embodiments will be apparent to those of skill in the art upon reviewing the above description. The scope of the invention should, therefore, be determined with reference to the appended claims, along with the full scope of equivalents to which such claims are entitled. In the appended claims, the terms “including” and “in which” are used as the plain-English equivalents of the respective terms “comprising” and “wherein.” Moreover, in the following claims, the terms “first,” “second,” and “third,” etc. are used merely as labels, and are not intended to impose numerical requirements on their objects. Further, the limitations of the following claims are not written in means-plus-function format and are not intended to be interpreted based on 35 U.S.C. §112, sixth paragraph, unless and until such claim limitations expressly use the phrase “means for” followed by a statement of function void of further structure.

This written description uses examples to disclose the invention, including the best mode, and also to enable any person skilled in the art to practice the invention, including making and using any devices or systems and performing any incorporated methods. The patentable scope of the invention is defined by the claims, and may include other examples that occur to those skilled in the art. Such other examples are intended to be within the scope of the claims if they have structural elements that do not differ from the literal language of the claims, or if they include equivalent structural elements with insubstantial differences from the literal languages of the claims. 

1. A distance measuring device comprising: a reflective member; and a sensor device having at least one coupling probe for feeding a transmission signal into a line structure with the reflective member, wherein the reflective member includes a base plate with an attached collar forming a generally cylindrical hollow shaped element, the attached collar comprising the coupling probe in an end position of the reflective member.
 2. The distance measuring device according to claim 1, wherein the attached collar includes a synthetic plate.
 3. The distance measuring device according to claim 1, further comprising a groove structure in a front face of the base plate and extending in a circumferential direction.
 4. The distance measuring device according to claim 3, wherein the groove structure comprises at least two grooves.
 5. The distance measuring device according to claim 3, further comprising a dielectric material filled within the grooves.
 6. The distance measuring device according to claim 1, further comprising a plastic ring formed in part by the collar at an end thereof.
 7. The distance measuring device according to claim 1, further comprising a plastic ring provided on an outer surface of the collar and including a surface pairing corresponding to the outer surface of the collar and extending conically.
 8. The distance measuring device according to claim 1, wherein the line structure includes a feed block with a coaxial feed region configured to connect an HF transceiver to a dielectric restraint system with the coupling probe via a wave guide.
 9. The distance measuring device according to claim 8, wherein the dielectric restraint system comprises a material with low water absorption and release and configured to be implemented at least one of solidly and in individual supports with cylinders with a large diameter.
 10. The distance measuring device according to claim 8, wherein the feed block includes boreholes into which the restraint system, the coupling probe and the coaxial feed region are configured to be inserted.
 11. The distance measuring device according to claim 1, wherein the line structure comprises a circular hollow conductor, having a cylinder with a piston as a reflective member.
 12. The distance measuring device according to claim 11, wherein the reflective member is attached to the piston.
 13. The distance measuring device according to claim 1, further comprising a cover configured to provide pneumatic pressure compensation.
 14. The distance measuring device according to claim 1, wherein the coupling probe is designed as a monopole stimulation system, and a feed of an electromagnet wave implemented coaxially and converted to the monopole with a multi-step coaxial transformation step.
 15. The distance measuring device according to claim 1, wherein the coupling probe is formed as a three-step transformation module having a level base on a center of which a cylinder is provided and to which a pin is attached such that a feed region is connected to the coupling probe.
 16. The distance measuring device according to claim 15, wherein the coupling probe is covered by a plastic material having a low water absorption and water release.
 17. The distance measuring device according to claim 1, wherein the coupling probe is configured to radiate the transmission signal as an electromagnetic wave in the high frequency range.
 18. The distance measuring device according to claim 17, wherein the high frequency range is between 100 MHz and 25 Hz.
 19. The distance measuring device according to claim 17, wherein the coupled electromagnetic wave includes a monomodal propagation in the E01 mode using the circular hollow conductor.
 20. The distance measuring device according to claim 1, wherein the coupling probe is configured to radiate at least two transmission signals as electromagnetic waves with different frequencies.
 21. The distance measuring device according to claim 20, wherein the coupled electromagnetic wave includes a monomodal propagation in a TEM mode with a coaxial structure.
 22. The distance measuring device according to claim 1, wherein the sensor device comprises high frequency electronics with a transmitting and receiving branch.
 23. The distance measuring device according to claim 22, wherein the high frequency electronics comprises phase locked loop (PLL), an oscillator (VCO), a mixer, frequency distributors and amplifiers integrated onto a common substrate.
 24. The distance measuring device according to claim 23, wherein a substrate material comprises one of silicium germanium, silicium, silicium germanium carbide and silicium carbide.
 25. The distance measuring device according to claim 1, further comprising analysis electronics and wherein at least one of the analysis electronics and the sensor device are configured as interface electronics, in a chip arrangement, and provided on a feed block.
 26. The distance measuring device according to claim 25, wherein the chip arrangement is configured to provide a transmitting and receiving frequency selectably adjusting a divider ratio by applying an external voltage in discrete steps.
 27. The distance measuring device according to claim 1, further comprising analysis electronics comprising digital signal processor (DSP), phase locked loop (PLL), memory implemented as a free programmable gate array (FPGA).
 28. The distance measuring device according to claim 1, further comprising interface electronics implemented both as an analog and digital bus, and having a pre-programmable gate array (FPGA) configured to allocate to the generation of an interface protocol and control of a digital to analogue conversion.
 29. A method for determining a distance, the method comprising: a) providing a line structure with a reflective member that has a feed block with a feed region that connects a high frequency (HF) transceiver to a dielectric restraint system with a coupling probe using a waveguide, wherein the reflective member has a base plate with an attached collar for forming a generally cylindrical hollow shaped element; and b) measuring the distance between a feed point defined by the coupling probe and the reflective member, wherein at least two transmission signals are coupled as electromagnetic waves with different frequencies radiated and received, via the coupling probe.
 30. The method according to claim 29, wherein the transmission signals are continuously radiated.
 31. The method according to claim 29, wherein three transmission signals are radiated as electromagnetic waves via the coupling probe.
 32. The method according to claim 29, further comprising measuring the distance based on a phase difference between the transmitted signal and the received signal of the electromagnetic wave.
 33. The method according to claim 32, wherein the difference of at least two transmission frequencies of the respective electromagnetic wave being about 1% of an absolute value thereof.
 34. The method according to claim 32, wherein the difference between the frequencies of the transmission signal of the respective electromagnetic wave being about 20% of an absolute value thereof. 